Flow distribution
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The concept Flow distribution represents the subject, aboutness, idea or notion of resources found in Houston Public Library.
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Flow distribution
Resource Information
The concept Flow distribution represents the subject, aboutness, idea or notion of resources found in Houston Public Library.
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- Flow distribution
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100+ Items that share the Concept Flow distribution
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- 16-foot transonic tunnel test section flowfield survey
- 1987 Ground Vortex Workshop : proceedings of a meeting held at NASA Ames Research Center, Moffett Field, California, April 22-23, 1987
- 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- A 2-D oscillating flow analysis in Stirling engine heat exchanges
- A CFD study of complex missile and store configurations in relative motion : final report for the period ended September 30, 1994
- A CFD study of tilt rotor flowfields
- A FORTRAN computer code for calculating flows in multiple-blade-element cascades
- A closure for the compressibility of the source terms in lighthill's acoustic analogy
- A combined experimental/computational study of flow in turbine blade cooling passage
- A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field
- A computational examination of directional stability for smooth and chined forebodies at High-¿
- A critical survey of optimization models for tactical and strategic aspects of air traffic flow management
- A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics
- A final report on NASA grant NGL-22-009-383 entitled Unsteady design-point flow phenomena in transonic compressors : final report
- A generalized fluid system simulation program to model flow distribution in fluid networks : draft paper ...
- A knowledge-based approach to automated flow-field zoning for computational fluid dynamics
- A model for closing the inviscid form of the average-passage equation system
- A multi-domain spectral method for supersonic reactive flows
- A note on trapping moving vortices
- A novel potential viscous flow coupling technique for computing helicopter flow fields
- A novel potential/viscous flow coupling technique for computing helicopter flow fields : final report
- A numerical study of chemically reacting flow in nozzles
- A numerical study of the effect of wake passing on turbine blade film cooling
- A parametric study of accelerations of an airplane due to a wake vortex system
- A parametric study of accelerations of an airplane due to a wake vortex system
- A planar reacting shear layer system for the study of fluid dynamics-combustion interaction
- A progress report for an ecological study of peat landforms in Canada and Alaska
- A qualitative and quantitative laser-based computer-aided flow visualization method
- A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone : final report
- A reduced order model of the linearized incompressible Navier-Strokes equations for the sensor/actuator placement problem
- A robust design methodology for optimal microscale secondary flow control in compact inlet diffusers
- A shadowgraphic study of the national launch system's 1 1/2 stage vehicle configuration and heavy lift launch vehicle configuration
- A simplified model for detonation based pressure-gain combustors
- A smoke generator system for aerodynamic flight research
- A steadying effect of acoustic excitation on transitory stall
- A study of Dean vortex development and structure in a curved rectangular channel with aspect ratio of 40 at Dean numbers up to 430
- A study of gas flow pattern, undercutting and torch modification in variable polarity plasms arc welding
- A study of the vortex flow over 76/40-deg double-delta wing
- A user's manual for ROTTILT solver : tiltrotor fountain flow field prediction
- A wall interference assessment/correction interface measurement system for the NASA-ARC 12-FT PWT : final memorandum report
- AST combustion workshop : working group report
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Acoustical and flowfield characterization of a scaled tabletop rocket
- Adaptive grid embedding for the two-dimensional flux-split Euler equations
- Additional development of the XTRAN3S computer program
- Advanced 3-D viscous SSME turbine rotor stator CFD algorithms 6 September 85 - 5 September 86 : final report
- Advanced noise control fan aerodynamic performance
- Advanced space propulsion system flowfield modeling : final report : contract NAS8-40845
- Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests)
- Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations
- Aerodynamic classification of swept-wing ice accretion
- Aerodynamic flow field measurements for automotive systems
- Aerodynamic performance of a compact, high work-factor centrifugal compressor at the stage and subcomponent level
- Aeropropulsion technology (APT) : task 23--stator seal cavity flow investigation
- Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
- Aerothermal tests of a 12.5° cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
- Air traffic management technology demonstration- 3 (ATD-3) multi-flight common route (MFCR) concept of operations : version 1.0
- Air-jet milling of grinding materials
- An LU implicit scheme for high speed inlet analysis
- An application of a two-equation model of turbulence to three-dimensional chemically reacting flows
- An approximate method for calculating three-dimensional inviscid hypersonic flow fields
- An arbitrary grid CFD algorithm for configuration aerodynamics analysis, Vol.1, Theory and validations
- An arbitrary grid CFD algorithm for configuration aerodynamics analysis, Vol.2, FEMNAS user guide
- An edge-based solution-adaptive method applied to the AIRPLANE code
- An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts
- An experimental documentation of trailing-edge flows at high Reynolds number
- An experimental investigation of steady and unsteady flow field in an axial flow turbine
- An experimental study of an adaptive-wall wind tunnel
- An experimental study of characteristic combustion-driven flow for CFD validation : final report for NASA contract NAS8-38862
- An experimental study of swirling flows as applied to annular combustors : a thesis ...
- An experimental study of the aerodynamics of a NACA 0012 airfoil with a simulated glaze ice accretion
- An experimental study of the flowfield on a semispan rectangular wing with a simulated glaze ice accretion
- An experimental study of the turbulent boundary layer on a transport wing in subsonic and transonic flow
- An investigation into the flow behavior of a single phase gas system and a two phase gas/liquid system in normal gravity with nonuniform heating from above
- An investigation of candidate sensor-observable wake vortex strength parameters for the NASA Aircraft Vortex Spacing System (AVOSS) : under cooperative agreement NCC1-24
- An oil flow study of the reference Shuttle-C configuration
- An upwind-differencing scheme for the incompressible Navier-Stokes equations
- Analyses of physical-chemical processes governing SSME internal fluid flows : progress report for November 1984
- Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
- Analysis of advanced solid rocket motor ignition phenomena : final report
- Analysis of coupled seals, secondary and powerstream flow fields in aircraft and aerospace turbomachines
- Analysis of inviscid and viscous flows in cascades with an explicit multiple-grid algorithm
- Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows
- Application of a self-adaptive grid method to complex flows
- Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers
- Application of computational fluid dynamics in high speed aeropropulsion
- Application of laser anemometry in turbine engine research
- Application of laser velocimetry to unsteady flows in large scale high speed tunnels
- Application of particle image velocimetry to a study of flow about a multi-element airfoil : final report for the period August 15, 1995 to August 14, 1996 ... grant no. NCC2-5155
- Approaches to validation of models for low gravity fluid behavior
- Assessment of a 3-D boundary layer analysis to predict heat transfer and flow field in a turbine passage
- Assessment of three-dimensional inviscid codes and loss calculations for turbine aerodynamic computations
- Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor
- Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor
- Autoclave processing for composite material fabrication. 1 An analysis of resin flows and fiber compactions for thin laminate
- Autoclave processing for composite material fabrication. 1. An analysis of resin flows and fiber compactions for thin laminate
- Automated fluid feature extraction from transient simulations : progress report
- Axis switching and spreading of an asymmetric jet : role of vorticity dynamics
- Boundary conditions for jet flow computations
- Boundary layer flow control by an array of ramp-shaped vortex generators
- CFD for hypersonic propulsion
- CFD research, parallel computation and aerodynamic optimization
- CFD study of NACA 0018 airfoil with flow control
- CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system : final report : under contract NAG3-1500
- Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests)
- Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
- Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications
- Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications
- Characterization of three-stream jet flow fields
- Coarse grid modeling of turbine film cooling flows using volumetric source terms
- Coarse grid modeling of turbine film cooling flows using volumetric source terms
- Comparison of the aeroacoustics of two small-scale supersonic inlets : final technical report, NASA contract #--NAG 3-1539
- Comparison of tomo-PIV versus dual plane PIV on a synthetic jet flow
- Computation of Navier-Stokes equations for three-dimensional flow separation
- Computation of lifting wing-flap configurations : NASA grant NCC2-5070, final report ... funding dates: July 1, 1994 to June 30, 1995
- Computation of separated and unsteady flows with one- and two-equation turbulence models : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV
- Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages
- Computation of viscous flow in curved ducts and comparison with experimental data
- Computational aerodynamic simulations of a 1215 ft/sec tip speed transonic fan system model for acoustic methods assessment and development
- Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development
- Computational aeroheating predictions for X-34
- Computational aspects of zonal algorithms for solving the compressible Navier-Stokes equations in three dimensions
- Computational fluid dynamics and aerothermodynamics : semiannual progress report, January 1987--June 1987
- Computational fluid dynamics and areothermodynamics : final report, January 1987--December 1988
- Computational investigation of tangential slot blowing on a generic chined forebody
- Computational methods for the problems of the tip vortex : final technical report
- Computational study of flow establishment in hypersonic pulse facilities
- Computational study of generic hypersonic vehicle flow field
- Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
- Computer code for predicting coolant flow and heat transfer in turbomachinery
- Computer codes for the evaluation of thermodynamic properties, transport properties, and equilibrium constants of an 11-species air model
- Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed
- Conjugate heat transfer analyses on the manifold for ramjet fuel injectors
- Contraction design for small low-speed wind tunnels
- Control of separated flow past a cylinder using tangential wall jet blowing
- Control of shear flows by artificial excitation
- Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel
- Corrections for attached sidewall boundary-layer effects in two-dimensional airfoil testing
- Correlation of puma airloads : evaluation of CFD prediction methods
- Current Lewis turbomachinery research : building on our legacy of excellence
- Current Lewis turbomachinery research : building on our legacy of excellence
- Data Parallel Line Relaxation (DPLR) code user manual : Acadia version 4.01.1
- Debris/ice/TPS assessment and integrated photographic analysis of shuttle mission STS-67
- Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel
- Design and analysis tool for external-compression supersonic inlets
- Design and calibration of the mixing layer and wind tunnel
- Detailed flow-field measurements over a 75° swept delta wing
- Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing
- Determination of the pressure drag of airfoils by integration of surface pressures
- Deterministic stress modeling of hot gas segregation in a turbine
- Development of a laser-induced heat flux technique for measurement of convective heat transfer coefficients in a supersonic flowfield
- Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle : final report
- Development of an actuator for flow control utilizing detonation
- Development of detonation modeling capabilities for rocket test facilities : hydrogen-oxygen-nitrogen mixtures
- Development of tripropellant CFD design code : contract no.--NAS8-40583 : final report
- Direct replacement of arbitrary grid-overlapping by non-structured grid
- Discrete-vortex model for the symmetric-vortex flow on cones
- Duct flow nonuniformities for space shuttle main engine (SSME) : final report
- Dynamic flow management problems in air transportation
- Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
- Effect of acoustic excitation on stalled flows over an airfoil
- Effect of area ratio on the performance of a 5.5:1 pressure ratio centrifugal impeller
- Effect of convection on the microstructure of a lamellar eutectic growing with a snapped interface
- Effect of delta tabs on free jets from complex nozzles
- Effect of delta tabs on free jets from complex nozzles
- Effect of jet exit vanes on flow pulsations in an open-jet wind tunnel
- Effect of passive venting on static pressure distributions in cavities at subsonic and transonic speeds
- Effect of sweep on cavity flow fields at subsonic and transonic speeds
- Effects of a forward-swept front rotor on the flowfield of a counterrotation propeller
- Effects of convection during the photodeposition of polydiacetylene thin films
- Effects of gravity on cocurrent two-phase gas-liquid flows through packed columns
- Effects of gravity on concurrent two-phase gas-liquid flows through packed columns
- Effects of inlet conditions on crossflow jet mixing
- Effects of inlet flow conditions on crossflow jet mixing
- Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows : progress report for the period ended December 31, 1989
- Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance
- Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825
- Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79
- Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Electron-beam diagnostic methods for hypersonic flow diagnostics : final NASA report grant no. 2-718
- Endwall heat transfer measurements in a transonic turbine cascade
- Endwall heat transfer measurements in a transonic turbine cascade
- Energy efficient engine : high pressure turbine component test performance report
- Engineering aerothermal analysis for X-34 thermal protection system design : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
- Enhanced line integral convolution with flow feature detection : NAS technical report NAS-96-007
- Equilibrium radiative heating tables for aerobraking in the Martian atmosphere
- Equilibrium radiative heating tables for earth entry
- Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
- Evaluation of non-intrusive flow measurement techniques for a re-entry flight experiment
- Evaluation of turbulence models for unsteady flows of an oscillating airfoil
- Evolution toward a decentralized air traffic flow management system : final report
- Evolutionary concepts for decentralized air traffic flow management
- Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes
- Experimental aerothermodynamic research of hypersonic aircraft : technical progress report (substitution) for the period October 1, 1988 - March 31, 1989
- Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft
- Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
- Experimental evaluation of the effect of angle-of-attack on the external aerodynamics and mass capture of a symmetric three-engine air-breathing launch vehicle configuration at supersonic speeds
- Experimental investigation of crater growth dynamics : semiannual report
- Experimental investigation of hypersonic aerodynamics : semi-annual research report for the period April 1, 1987 - September 30, 1987
- Experimental investigation of the flow field in a transonic, axial flow compressor, with respect to the development of blockage and loss
- Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 : final report
- Experimental investigation of wing installation effects on a two-dimensional mixer/ejector nozzle for supersonic transport aircraft
- Experimental results for a hypersonic nozzle/afterbody flow field
- Experimental study of saddle point of attachment in laminar juncture flow
- Experimental visualization of flows in packed beds of spheres
- Experimental visualization of flows in packed beds of spheres
- Experiments on the flow field physics of confluent boundary layers for high-lift systems
- Experiments on two opposed lateral jets injected into swirling crossflow
- Exploratory flow visualization investigation of mast-mounted sights in presence of a rotor
- Exploring a method for improving turbulent separated-flow predictions with [k-omega] models
- Extension of a streamwise upwind algorithm to a moving grid system
- Extension of a three-dimensional viscous wing flow analysis
- F/A-18 forebody vortex control
- Final report on investigation of transonic flow over segmented slotted wind tunnel wall with mass transfer
- Final report, entitled, Data reduction and analysis of Pioneer Venus Orbital Ion Mass Spectrometer : NASA grant NAG 2-566, covering the period October 1998 - March 1996
- Final technical report for Euler/Navier-Stokes solvers applied to ducted fan configurations : NASA grant number NAG3-1230 : grant duration, December 20, 1990 to December 20, 1996
- Flight survey of the 757 wing noise field and its effects on laminar boundary layer transition, Vol. I, Program description and data analysis
- Flight test results from the rake airflow gage experiment on the F-15B airplane
- Floating shock fitting via lagrangian adaptive meshes
- Flow distribution around the SSME main injector assembly using porosity formulation
- Flow duct data for validation of acoustic liner codes for impedance education
- Flow field around a hovering rotor
- Flow field characterization of an angled supersonic jet near a bluff body
- Flow field survey near the rotational plane of an advanced design propeller on a Jetstar airplane
- Flow fields of low pressure vent exhausts
- Flow in rotating serpentine coolant passages with skewed trip strips : under contract NAS3-27378
- Flow in serpentine coolant passages with trip strips : technical progress narrative report, reporting period September 1, 1995 to September 30, 1995
- Flow induced vibrations in the SSME injector heads : final report no. RI/RD 91-157
- Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests)
- Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests)
- Flow simulation in secondary flow passages of a rocket engine turbopump : draft paper for 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 13-15, 1998, Cleveland, Ohio
- Flow through very porous screens
- Flow through very porous screens
- Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles
- Flow visualization studies of VTOL aircraft models during hover in ground effect
- Flow visualization techniques for flight research
- Flow-field survey of an empennage wake interacting with a pusher propeller
- Flow-field surveys for rectangular nozzles
- Flowfield computation of entry vehicles
- Flowfield of a lifting hovering rotor--a Navier-Stokes simulation
- Flowfield-dependent mixed explicit-implicit (FDMEI) algorithm for computational fluid dynamics : final report ...
- Flows in pinned arrays simulating brush seals
- Flows in pinned arrays simulating brush seals
- Foundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines
- Fundamental study of flow field generated by rotorcraft blades
- Fuzzy interference enhanced information recovery from digital PIV using cross-correlation combined with particle tracking
- Global flowfield about the V-22 tiltrotor aircraft : final report of NASA cooperative agreement NCC2-747
- Global flowfield about the V-22 tiltrotor aircraft : progress report for NASA cooperative agreement NCC2-747
- Ground effects on V/STOL and STOL aircraft--a survey
- Growth characteristics downstream of a shallow bump : computation and experiment
- HPFTP flow diverter analysis : monthly progress report
- Harmonic balance computations of fan aeroelastic stability
- Heat entrapment effects within liquid acquisition devices
- Heat entrapment effects within liquid acquisition devices
- Hi-alpha forebody design
- High frequency flow/structural interaction in dense subsonic fluids
- High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment : final report
- High pressure turbine test hardware detailed design report
- High speed turboprop aeroacoustic study (counterrotation), Volume 1, Model development
- High-altitude plume computer code development : final report
- High-altitude plume computer code development : final report
- Holographic aids for internal combustion engine flow studies
- Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel
- Hybrid propulsion for launch vehicle boosters : a program status update
- Hypersonic flows as related to the national aerospace plane
- Hypervelocity atmospheric flight : real gas flow fields
- ICEG2D (v2.0) : an integrated software package for automated prediction of flow fields for single-element airfoils with ice accretion
- Ice particle transport analysis with phase change for the E3 turbofan engine using LEWICE3D version 3.2
- Identification and characterization of key human performance issues and research in the Next Generation Air Transportation System (NextGen)
- Implementation of an associative flow rule including hydrostatic stress effects into the high strain rate deformation analysis of polymer matrix composites
- Improved two-equation k - [omega] turbulence models for aerodynamic flows
- Improving jet reactor configuration for production of carbon nanotubes
- Influence of two-phase thermocapillary flow on cryogenic liquid retention in microscopic pores
- Injector mixing efficiency experiments : final report : contract number NAS8-38609 D.O. 159
- Inlet flow control and prediction technologies for embedded propulsion systems : summary report for fiscal year 2009
- Inlet flow test calibration for a small axial compressor facility, Part I, Design and experimental results
- Inlet flowfield investigation, Part I, Transonic flowfield survey
- Inlet flowfield investigation, Part II., Computation of the flow about a supercruise forebody at supersonic speeds
- Interactive grid generation for turbomachinery flow field simulations
- Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
- Investigation of advanced counterrotation blade configuration concepts for high speed turboprop systems : final report, Task 1, Ducted propfan analysis
- Investigation of chemically-reacting supersonic internal flows
- Investigation of empennage buffeting : technical report CRINC-FRL-714-1
- Investigation of mixing a supersonic stream with the flow downstream of a wedge : NCC2-5190 final report
- Investigation of wing upper surface flow-field disturbance due to NASA DC-8-72 in-flight inboard thrust-reverser deployment
- Jet noise reduction potential from emerging variable cycle technologies
- Jet vortex generators for turbulent flow separation control
- Key topics for high-lift research : a joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996
- LAURA users manual, 5.3-48528
- Large perturbation flow field analysis and simulation for supersonic inlets : final report
- Large-eddy simulation of laminar-turbulent breakdown at high speeds with dynamic subgrid-scale modeling
- Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller
- Laser anemometer measurements of the flow field in a 4:1 pressure ratio centrifugal impeller
- Laser anemometer measurements of the three-dimensional rotor flow field in the NASA low-speed centrifugal compressor
- Laser transit anemometer measurements on a slender cone in the Langley unitary plan wind tunnel
- Lateral jet injection into typical combustor flowfields
- Local and global bifurcations of flow fields during physical vapor transport : application to a microgravity experiment
- Local and global bifurcations of flow fields during physical vapor transport : application to a microgravity experiment
- Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds
- Low speed calibration of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1995 test) : under contract NAS3-27186
- Low-speed flowfield characterization by infrared measurements of surface temperatures
- Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Mach 5 inlet CFD and experimental results
- Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Mach 6 flow field surveys beneath the forebody of an airbreathing missile
- Mach number and flow-field calibration at the advanced design propeller location on the JetStar airplane
- Magnetohydrodynamic and gasdynamic theories for planetary bow waves
- Material processing of convection-driven flow field and temperature distribution under oblique gravity : annual report
- Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet
- Measurements and modeling of flow structure in the wake of a low profile "wishbone" vortex generator
- Measurements and simulations of surface dielectric barrier discharges used as plasma actuators, final report
- Measurements of a turbulent horseshoe vortex formed around a cylinder
- Measurements of a turbulent horseshoe vortex formed around a cylinder
- Measurements of a turbulent horseshoe vortex formed around a cylinder
- Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage
- Measurements of store forces and moments and cavity pressures for a generic store in and near a box cavity at subsonic and transonic speeds
- Measurements of turbulent flow field in separate flow nozzles with enhanced mixing devices, test report
- Micro-ramp flow control for oblique shock interactions : comparisons of computational and experimental data
- Navier-Stokes calculations for a highly-twisted rotor near stall
- Navier-Stokes flow field analysis of compressible flow in a high pressure safety relief valve
- Near-field noise of a single-rotation propfan at an angle of attack
- Near-wall modelling of compressible turbulent flows : a semi-annual progress report
- Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields : semiannual progress report, February 1991 - June 1991
- Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields : semiannual progress report, January 1990--June 1990
- Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields, Volume II
- Nonisentropic unsteady three dimensional small disturbance potential theory
- Nonlinear dynamics of a diffusing interface
- Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
- Numerical analysis of intra-cavity and power-stream flow interaction in multiple gas-turbine disk-cavities
- Numerical analysis of tangential slot blowing on a generic chined forebody
- Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
- Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
- Numerical assessment of four-part through-flow wave rotor cycles with passage height variation
- Numerical assessment of four-port through-flow wave rotor cycles with passage height variation
- Numerical flow visualization in basic- and hyper-cluster spheres
- Numerical flow visualization in basic- and hyper-cluster spheres
- Numerical investigation of hot gas ingestion by STOVL aircraft : prepared under grant NAG3-1026
- Numerical investigations in the backflow region of a vacuum plume : performance report, May 1994 - August 1995
- Numerical investigations in three-dimensional internal flows : semi-annual status report, 1 April through 30 September 1988
- Numerical mixing calculations of confined reacting jet flows in a cylindrical duct
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part I, Fuel nozzle/rich-burn zone analysis
- Numerical simulation of a low emissions gas turbine combustor using KIVA-II, Part II, Quick-quench/lean-combustion zones analysis
- Numerical simulation of helicopter engine plume in forward flight : final report cooperative agreement #NCC2-5061
- Numerical simulation of particle-wave interaction in boudary layers : final report for NAG-1-798
- Numerical simulation of supersonic and hypersonic inlet flow fields : final report
- Numerical simulation of supersonic flow using a new analytical bleed boundary condition
- Numerical simulation of the SOFIA flow field
- Numerical simulations of the flow in the HYPULSE expansion tube
- Numerical solution of three-dimensional unsteady transonic flow over wings including viscid/viscous interactions
- Numerical solutions of Navier-Stokes equations for a Butler wing : progress report for the period ending August 31, 1985
- Numerical solutions of the complete Navier-Stokes equations : final report : NASA grant NAG-1-244
- Numerical study of steady and unsteady canard-wing-body aerodynamics
- Nummerical studies of interacting vortices
- On approximate factorization schemes for solving the full potential equation
- On approximate factorization schemes for solving the full potential equation
- On automating domain connectivity for overset grids : progress report for NASA grant 2-783
- On computations of the integrated space shuttle flowfield using overset grids : final report
- On hammershock propagation in a supersonic flow field
- On multiple-layered vortices
- On the coupling of CDISC design method with FPX rotor code
- On the receptivity and non-parallel stability of traveling disturbances in rotating disk flow
- Optical and probe determination of soot concentrations in a model gas turbine combustor
- Optimum shape of a blunt forebody in hypersonic flow
- Parallel ALLSPD-3D : speeding up combustor analysis via parallel processing
- Passage-averaged description of wave rotor flow
- Passive rocket diffuser testing : reacting flow performance of four second-throat geometries
- Passive rocket diffuser theory : a re-examination of minimum second throat size
- Performance improvement through indexing of turbine airfoils, Part 2, Numerical simulation
- Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating flow wind tunnel : progress report
- Performance tests for the NASA Ames Research Center 20 cm x 40 cm oscillating wind tunnel : progress report
- Phase averaged measurements of the coherent structure of a Mach number 0.6 jet
- Physical vapor transport of mercurous chloride under a nonlinear thermal profile
- Physics based model for cryogenic chilldown and loading, part IV, Code structure
- Pitot-pressure measurements in flow fields behind a rectangular nozzle with exhaust jet for free-stream mach numbers of 0.00, 0,60, and 1.20
- Plume dispersion of the exhaust from a cryogenic wind tunnel
- Predicting modes of the unsteady vorticity field near the trailing edge of a blade
- Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
- Pressure probe designs for dynamic pressure measurements in a supersonic flow field
- Pressure-distribution measurements on a transonic low-aspect ratio wing
- Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane
- Propulsion/airframe interference for ducted propfan engines with ground effect
- RNS applications for interacting sub- and supersonic flows : final report, NASA grant no. NAG1-1553, 11/19/93-5/18/97
- RSRM 10% Scale Model drilled hole plate tests : final report, contract NAS8-40347
- Radial and circumferential flow surveys at the inlet and exit of the Space Shuttle Main Engine High Pressure Fuel Turbine model
- Radiation from advanced solid rocket motor plumes
- Radiative coupled nonequilibrium flow fields associated with aeroassisted orbital transfer : final contractors report, July 1984 - March 1986
- Radiative interactions in chemically reacting compressible nozzle flows using Monte Carlo simulations
- Rapid calibration of seven-hole probes
- Rapid numerical simulation of viscous axisymmetric flow fields
- Rarefied gas effects on aerobraking/reentry vehicles with wakes
- Real gas effects on the performance of hydrocarbon-fueled pulse detonation engines
- Real-gas flow properties for NASA Langley Research Center Aerothermodynamic Facilities Complex wind tunnels : under grants NAG1-1663 and NAGW-1331
- Reconstruction of a three-dimensional transonic rotor flow field from holographic interferogram data
- Reliability enhancement of Navier-Stokes codes through convergence acceleration : final report
- Response of high subsonic jet to nonaxisymmetric disturbances
- Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310)
- Review of blunt body wake flows at hypersonic low density conditions
- Review of blunt body wake flows at hypersonic low density conditions
- Rocket-based combined cycle engine technology development : inlet CFD validation and application
- SSME LOX post flow analysis/fluid structure interaction : final report
- SSME LOX post flow analysis/fluid structure interaction, Volume 1, Flow analysis : final report
- SSME fuelside preburner two-dimensional analysis
- SSME main combustion chamber and nozzle flowfield analysis : final report
- Schlieren system and method for moving objects
- Self-compensating solenoid valve
- Self-recirculating casing treatment concept for enhanced compressor performance
- Semianalytic modeling of aerodynamic shapes
- Semidiscrete Galerkin modelling of compressible viscous flow past a circular cone at incidence
- Sensitivity analysis for aeroacoustic and aeroelastic design of turbomachinery blades : final technical report
- Shear layer excitation, experiment versus theory
- Simulation and modeling of homogenious, compressed turbulence
- Simulation of pressure and temperature responses for the 20 inch supersonic wind tunnel
- Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral
- Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral
- Simulation of unsteady hypersonic combustion around projectiles in an expansion tube
- Simulations of spray reacting flows in a single element LDI injector with and without invoking an Eulerian scalar PDF method
- Solution of Poisson equations for three-dimensional grid generations
- Solutions to three-dimensional thin-layer Navier-Stokes equations in rotating coordinates for flow through turbomachinery
- Space shuttle ice suppression system validation : volume I
- Special opportunities in helicopter aerodynamics
- Stability of a non-orthagonal stagnation flow to three dimensional disturbances
- Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
- Structure of a swirl-stabilized combusting spray
- Structure of a swirl-stabilized combusting spray
- Study of CFD methods applied to rapidly deforming boundaries
- Study of the integration of wind tunnel and computational methods for aerodynamic configurations
- Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration
- Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
- Summary of in-flight flow visualization obtained from the NASA high alpha research vehicle
- Summary of pressure gain combustion research at NASA
- Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
- Supersonic reacting internal flow fields
- Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2
- Surface tension driven convection experiment (STDCE)
- Survey of turbulence models for the computation of turbulent jet flow and noise
- System identification and POD method applied to unsteady aerodynamics
- The F/A-18 high-angle-of-attack ground-to-flight correlation : lessons learned
- The F/A-18 high-angle-of-attack ground-to-flight correlation, lessons learned
- The aerodynamic characteristics of vortex ingestion for the F/A-18 inlet duct
- The boundary layer on compressor cascade blades
- The boundary layer on compressor cascade blades
- The design/analysis of flows through turbomachinery : a viscous/inviscid approach
- The determination of the large-scale circulation of the Pacific Ocean from satellite altimetry using model Green's functions
- The effect of wake passing on turbine blade film cooling
- The effect of wake passing on turbine blade film cooling
- The effects of forcing on a single stream shear layer and its parent boundary layer
- The effects of vortex ingestion on the flow in a diffusing S-DUCT
- The influence of jet-grid turbulence on heat transfer from the stagnation region of a cylinder in crossflow
- The physics of turbulence in the boundary layer : final report ... NASA grant NAG-1-1610
- The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
- The use of oil for in-flight flow visualization
- Theoretical and experimental flow fields for a supersonic cruise fighter forebody
- Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels
- Theory of finite disturbances in a centrifuglal compression system with a vaneless radial diffuser
- Three-dimensional Euler time accurate simulations of fan rotor-stator interactions
- Three-dimensional effects on airfoils
- Three-dimensional flow field measurements in a transonic turbine
- Three-dimensional flow field measurements in a transonic turbine cascade
- Three-dimensional self-adaptive grid method for complex flows
- Three-dimensional structure in a supersonic jet : behavior near centerline
- Thrust measurement of Dielectric Barrier Discharge (DBD) plasma actuators : new anti-thrust hypothesis, frequency sweeps methodology, humidity and enclosure effects
- Towards a comprehensive computational simulation system for turbomachinery
- TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations : theory document
- Transition and turbulence modeling for blunt-body wake flows : abstract of paper proposed for the 32nd AIAA Thermophysics Conference, June 23-25, 1997, Atlanta, Georgia
- Transition mixing study final report
- Turbine blade-tip clearance excitation forces : final report on Contract number NAS8-35018
- Turbulence and pressure loss characteristics of the inlet vanes for the 80-by 120-foot wind tunnel
- Turbulence modeling for sharp-fin-induced shock wave/turbulent boundary-layer interactions
- Turbulence modeling validation, testing, and development
- Turbulence modeling validation, testing, and development
- Turbulence modelling of flow fields in thrust chambers : final technical report for the period June 10, 1991 through September 13, 1992
- Turbulence structures associated with the bursting event
- Turbulent chemical interaction models in NCC : comparison
- Turbulent inflow measurements : final report, grant number L-1625, period covered: 5 July 1995 to 31 December 1996
- Turbulent transport models for scramjet flowfields
- Two phase flow modeling : summary of flow regimes and pressure drop correlations in reduced and partial gravity
- Two-dimensional Euler and Navier Stokes time accurate simulations of fan rotor flows
- Understanding and mitigating tip leakage and endwall losses in high pressure ratio cores
- Understanding the flow physics of shock boundary-layer interactions using CFD and numerical analyses
- Unsteady blade-surface pressures on a large-scale advanced propeller : prediction and data
- Unsteady flow field in a multistage axial flow compressor
- Unsteady potential flow past a propeller blade section
- Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel
- User's guide for NASCRIN--a vectorized code for calculating two-dimensional supersonic internal flow fields
- User's manual for three dimensional boundary layer (BL3-D) code
- V/STOL wind-tunnel testing
- Vibrational power flow analysis of rods and beams
- Visualization of flows in packed beds of twisted tapes
- Visualization of flows in packed beds of twisted tapes
- Visualizing time-varying phenomena in numerical simulations of unsteady flows
- Visualizing vector fields using line integral convolution and dye advection
- Vortex interaction with a leading-edge of finite thickness
- Wake flow about the Mars Pathfinder entry vehicle
- Wake measurements in a strong adverse pressure gradient
- Water flow measurements in a 180 degree turn-around duct
- Water tunnel flow visualization study through poststall of 12 novel planform shapes
- Water-tunnel study results of a TF/A-18 and F/A-18 canopy flow visualization
- Wind code application to external forebody flowfields with comparisons to experimental results
- Wind code application to external forebody flowfields with comparisons to experimental results
- Wind tunnel seeding systems for laser velocimeters
- Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena
- Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes
- Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing
- Zero side force volute development : final report
- [Numerical computation of viscous flow around bodies and wings moving at supersonic speeds] : final report, NASA grant NGR 16-002-003, November 15, 1971 - March 31, 1984
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.houstonlibrary.org/resource/eiXoSiGEMdU/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.houstonlibrary.org/resource/eiXoSiGEMdU/">Flow distribution</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.houstonlibrary.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.houstonlibrary.org/">Houston Public Library</a></span></span></span></span></div>
